| Name of Satellite, Alternate Names | Saudisat 1C (Oscar 50, SO 50) |
| Country of Operator/Owner | Saudi Arabia |
| Operator/Owner | Space Research Institute, King Abdulaziz City for Science and Technology |
| Users | Government |
| Purpose | Research |
| Class of Orbit | LEO |
| Type of Orbit | Intermediate |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 603 |
| Apogee (km) | 702 |
| Eccentricity | 0.00704877180491278 |
| Inclination (degrees) | 64.6 |
| Period (minutes) | 97.8 |
| Launch Mass (kg.) | 10 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 20-12-2002 |
| Expected Lifetime | |
| Contractor | Space Research Institute, King Abdulaziz City for Science and Technology |
| Country of Contractor | Saudi Arabia |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Dnepr |
| COSPAR Number | 2002-058C |
| NORAD Number | 27607 |
| Comments | Microsatellite; carries several experiments, available to amateurs as power permits. |